01.2 - Aircraft Design and Integrated System (Applications)
PRELIMINARY DESIGN EXPLORATION OF PROSPECTIVE MULTIROTOR AEROBOTS FOR MARS
V. Youhanna¹, L. Felicetti¹, D. Ignatyev¹; ¹Cranfield University, United Kingdom
This preliminary design exploration assesses rotorcraft configurations for Martian exploration within defined parameters. Analysis includes single, dual, and quad rotorcrafts, focusing on power consumption in hover, climb, and forward flight. Findings highlight quad rotorcrafts' efficiency but underscore practical constraints. The study aids Martian aerobot designers in optimal configuration selection.